Solve Integral of dp^2 | Lower Boundary Ps, Upper P0

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intgral of dp^2??

Hi,

I have the following equation:

[itex]\dot{m} = c \frac{dp^{2}}{dx}[/itex]

Integration gives:

[itex]\dot{m} \int dx = c \int dp^{2}[/itex]

How can I solve [itex]\int dp^{2}[/itex]??

The lower boundary is Ps and the upper boundary is P0 for the integral!
 
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Hi tiny-tim ;-)

I want to integrate dp^2! So you take some parameter q and say that this parameter q is equal to p^2 and then solve the integral of dq instead of dp^2. This gives q again and thus p^2! Then fill in the upper and lower boundary for p: P0^2 - Ps^2

Am I right?
 


My original question is how to solve this equation:

[itex]\dot{m} \int dx = c \int dp^{2}[/itex]

My problem is solving the right hand side of the equation namely:

[itex]c \int dp^{2}[/itex]

Your answer is: replace [itex]p^{2}[/itex] by q and solve this 'normal' integral [itex]c \int dq[/itex]! This gives c q, then replace q by [itex]p^{2}[/itex] again so the solution is c [itex]p^{2}[/itex]. Then I only have to fill in the boundaries for p. Right?
 


dp²/dx is an infinitesimal quantity. On the left side of equation, you have a finite quantity. Something is wrong.

You either have (dp/dx)² or d²p/dx². In either case, review your equation. Where do you get it from, anyways?
 


Hi K^2,

This equation comes from Darcy's law namely [itex]\dot{m} = \frac{p Q}{R T}[/itex]

Fill Q (volumetric flow rate form Darcy's law) in in the above equation gives:

[itex]\dot{m} = c p \frac{dp}{dx}[/itex]

With [itex]c[/itex] all the constants in the equation.

[itex]p \frac{dp}{dx}[/itex] is equal to [itex]\frac{1}{2} \frac{dp^2}{dx}[/itex]

And thus finally I got [itex]\dot{m} = \frac{c}{2} \frac{dp^2}{dx}[/itex]

Solving this:

[itex]\dot{m} \int dx = \frac{c}{2} \int dp^{2}[/itex]

Therefore my question: How to solve [itex]\int dp^{2}[/itex] ??
 
ah, now i see where it comes from! :rolleyes:

yes, the whole point of changing pdp/dx to 1/2 d(p2)/dx

(and btw, it's better to write it that way, with brackets)

is because that is a perfect derivative, and you can immediately integrate it to pf2 - pi2. :smile:

Incidentally, the same trick enables us to go from F = ma (in mechanics) via a = vdv/dx to ∆(1/2 mv2) :wink:
 


Tiny-tim,

Do I make a fault against the mathematics by saying that [itex]\dot{m} = \frac{c}{2} \frac{dp^2}{dx}[/itex] can be solved through [itex]\dot{m} \int dx = \frac{c}{2} \int dp^{2}[/itex]??

Then still my question is: how to solve the right hand site of this equation namely the integral of [itex]\int dp^{2}[/itex] ??
 


Yeah, you shouldn't write it as dp²/dx, because that means (dp)²/dx, and that just isn't right. d(p²)/dx, on the other hand, does make sense, and d(p²) can be integrated over using variable substitution.

[tex]\int f(u)du = \int f(x)\frac{du}{dx}dx[/tex]

Which in this case, turns integral over d(p²) into integral over 2p dp.
 
hi hermano! :smile:

(btw, we say "a fault in the mathematics" … though you can say "a crime against mathematics"! :biggrin:)
hermano said:
Do I make a fault against the mathematics by saying that [itex]\dot{m} = \frac{c}{2} \frac{dp^2}{dx}[/itex] can be solved through [itex]\dot{m} \int dx = \frac{c}{2} \int dp^{2}[/itex]??

No, we often treat a derivative exactly like a fraction, and multiply both sides by dx (and then integrate) …

that's fine :smile:
Then still my question is: how to solve the right hand site of this equation namely the integral of [itex]\int dp^{2}[/itex] ??

∫ d(p2) = [p2] :wink:
 


Thanks, now it is clear for me!

Maybe you both can help me with another small issue I'm facing with this equation! For the integral of my pressure, I have to fill in the upper and lower boundary for p^2! However, I doubt of the input pressure is my upper or lower boundary, and also the same for the output pressure. What tells me which pressure (input - output) is the upper and lower boundary for my integral?

The equation gives the mass flow through a pipe (Poiseuille) from the high input pressure to the lower ouput pressure.